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035   $a(CKB)5470000002504040
035   $a(OCoLC)1104148291
035   $a(EXLCZ)995470000002504040
100   $a20190610d1948      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8 /$fby W.F. Lindsey, D.B. Stevenson, and Bernard N. Daley
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1948.
215   $a1 online resource (86 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1546
300   $a'September 1948."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 14).
517 3 $aAerodynamic characteristics of twenty four National Advisory Committee for Aeronautics 16-series airfoils at Mach numbers between 0.3 and 0.8
606   $aAerodynamics
606   $aAerofoils
606   $aWind tunnel testing
606   $aAerodynamics$2fast
606   $aAerofoils$2fast
606   $aWind tunnel testing$2fast
615  0$aAerodynamics.
615  0$aAerofoils.
615  0$aWind tunnel testing.
615  7$aAerodynamics.
615  7$aAerofoils.
615  7$aWind tunnel testing.
700   $aLindsey$b W. F.$01410527
702   $aDaley$b Bernard N.
702   $aStevenson$b D. B.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713764203321
996   $aAerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8$93499375
997   $aUNINA